T216 Specification
Power Output..............................….….……………………………………………………………………....100
HP
RPM...........................….……………………………………………………………......................40,000
(Est.)
Compressor.............….……………………………........................Single Stage Centrifugal
Impeller
Air Mass Flow.......................….………………………………………………………………………………..........N/A
Pressure
Ratio..............….……………………………………………………………………......................3 (Est.)
Combustion
Chamber....….………………...................Reverse Flow Single Can with Torus Scroll
Turbine.........................….……………………………………………………………....................Radial
Inflow
Layout..........................Single Spool Overhung with Reduction Gearbox.
3,600 rpm Output
Starting.......................….………………………………………………………………......................Hand
Crank
Ignition..................................................High Energy Exciter
with Generator, Pilot Burner
Fuel System.................….…;…………………………………………….......Hydro-
Lubrication..................................….………………………………………......Wet
Sump Return System
Oil Spec.............................….…………………………………………………...............0-
Accessories......................….……………………………………………………………………………...............None
Weight.......................….………………………………………………………………………........................50
kg
Application..........................................Industrial Stationary Engine,
Fire Pump, Education
Fuel Consumption..........….…………………………………………………………………………….....................N/A
Dimensions.................….……………………………………………………........................3'
Square Approx
Klöckner-
T312 Specification
Power Output..............................….….……………………………………………………………………....140
HP
RPM...........................….……………………………………………………………......................64,000
(Est.)
Compressor.............….……………………………........................Single Stage Centrifugal
Impeller
Air Mass Flow.......................….………………………………………………………………………………..........N/A
Pressure
Ratio..............….……………………………………………………………………......................4 (Est.)
Combustion
Chamber....….……………….…..........Reverse Flow Annular with Vaporising Burners
Turbine.........................….……………………………………………………………………..........two-
Layout....................….………………………………..……..single shaft with reduction gear
at hot end
Starting.......................….…………………………………………………………………………………..electric
starter
Ignition......................................….…………………………........High Energy
Exciter, Pilot Burner
Fuel System.................….…;…………………………………………….......Hydro-
Lubrication........…………….…dry-
Oil Spec.............................….……………………………………………………….……………….......Mil-
Accessories......................….……………………………………………………………………………...............None
Weight.......................….………………………………………………………………………........................30
kg
Application.............................….………...secondary power system APU(SPS)
on Tornado Jet
Fuel Consumption..........….…………………………………………………………………………….....................N/A
Another hand-
The magnificent but complex T312 is a single shaft APU designed for aircraft. One
of a family of small but powerful power plants and the only one to be mass produced
for fitment to the Tornado multi-
An intricate and complex engine originally fitted with a two stage compressor, later
versions used just a single re-
The T312 APU formed part of the Tornado Secondary Power System (SPS), when on the ground the aircraft systems could be driven by the APU independently of the main engines (RB199) and also used for starting them.
Deutz T216 Layout
KHD T312 Mechanical Layout
Klöckner-
KHD T117 Turbojet Engine-
KHD T117 Specification
Power Output...........................….………………………..........Up to 236 Lbs thrust
RPM..........................................….……………….....45,000
estimated maximum
Compressor...........….……...Centrifugal Impeller PR 5.5:1 Mass Flow
1.6kg/sec
Combustion Chamber...…......Reverse Flow Annular with 12 vaporising burners
Turbine.......................….……...........….………………………….....1
Stage Axial Flow
Layout.....................….….….......Single Spool with Accessory
Gearbox in Nose
Starting.....................….….......….………………………………..........Air
Impingement
Ignition................................….……………............Tourch Igniter
with HT Plug
Fuel System............................Engine Driven Gear Pump , Electronic
Control
Lubrication...............Return System, Engine Driven Gear Pump, Integral
Tank
Oil Spec.................................….…………………........Aeroshell 390, MIL-
Accessories..........................….………………...........Alternator
mounted in nose
Weight.................................….………………………………………………….............23Kg
Application........................................……………….……………..Target
Drone/RPV
Klöckner-
Below Magnificent: The Rotor system from the MK2 KHD T312 SPS